Pratt & Whitney PW2037
Service difficulty reports · 12,809
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'PW2037' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'PW2037' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA2013101792151Lever · out of adjustDOOR 4L ARMING HANDLE DOES NOT GO ALL THE WAY TO ARMED POSITION. ADJUSTED ARM LEVER POSITION, OPERATIONS CHECKED OK IAW MM.SDR CALA2013101792152Cam · faultyDOOR NR 1R WILL NOT OPEN FROM THE OUTSIDE & BUTTERFLY HANDLES WILL NOT STOW. REMOVED DOOR HANDLES, FOUND OUTER SHAFT BINDING ON BEARING, TORQUED NUT, REASSEMBLED TO MM 52-11-13 STEP L PG 208, FAILED INSPECTION. REMOVED AGAIN FOUND PEDESTAL CRACKED & SPACER &SDR CALA2013101792162Battery · faultyAPU NOT STARTING. REPEAT APU STARTING PROBLEM WITH NO INDICATED FAULTS NOTED. TROUBLE SHOOTING FOUND CHARGER & BATTERY AT FAULT. REPLACED APU BATTERY IAW MM 24-31-03 & REPLACED APU BATTERY CHARGER IAW MM 24-31-04. SYSTEM OPERATIONS CHECKED GOOD. APU STARTSDR CALA2013102192202Fuel Line · leakingLT WING HAS EVIDENCE OF FUEL LEAKING OUT OF TWO DRY BAY DRAIN HOLES.. REPLACED MAIN ENG FUEL LINE THRU DRY BAY, LEAK CHECKED OK.SDR CALA2013101792144Seat Track · damagedCABIN SEAT TRACK BS 400 RBL 24.5 HAS A PREVIOUS BLEND ON UPPER FLANGE. R & R SEAT TRACK IAW DRAWING 141N5131.SDR CALA2013101592075Light · defectiveCAPT & CTR FLUORESCENT TUBES STROBE AT LOW INTENSITIES. RELAMPED & CHECKED OKAY.SDR CALA2013101692100Unknown · malfunctionedLT FUEL TANK INDICATOR BLANK ON WING & COCKPIT INDICATOR. SUSPECT WIRING.SDR CALA2013101692107Light · unsecureFLOOR LIGHTING AT EXIT ROW 12ABC IS NOT ALL THE WAY DOWN. SECURED EMERGENCY EXIT LIGHT STRIP.SDR CALA2013101692113Sign · brokenLT WING OVER EXIT SIGN FRAME LOWER PORTION BROKEN. PREVIOUS REPAIR ATTEMPT FAILED. REPAIRED EXIT SIGN LOWER PORTION.SDR CALA2013101692115Panel · crackedPREVIOUS REPAIR CRACKED. BULLNOSE OF LE OF WING, LT HAND SIDE ABOUT 5 FT FROM ENG PYLON UNDER NR 5 SLAT. REPAIRED DAMAGED PANEL IAW AMM 57-40-99 & SRM 57-41-01.SDR CALA2013103192544Drain · cloggedWATER DRAINING OUT OF THE BELLY DRAIN HOLE. CHECKED AFT GLY DRAINAGE OPERATION IAW AMM & APPEARS OPERATION IS NORMAL. DOOR DRAINS & AFT FLOOR DRAIN COME OUT OF BELLY WEEP HOLE BY THE AFT DRAIN MAST & LAVATORY SVC PANEL. GALLEY SINK COMING OUT OF DRAIN MAST.SDR CALA2013101592072Servo Valve · leakingFLUID APPEARS TO BE LEAKING FROM THE SPOILER ACTUATOR ON THE 3RD ONE IN FROM THE LT WINGTIP. REPLACED ELECTROHYDRAULIC SERVOVALVE ON NR 3 SPOILER PCA IAW MM. OPERATIONS & LEAK CHECKED GOOD.SDR CALA2013101592077Light · inoperative2L SLIDE ARM LIGHT INOPERATIVE. RELAMPED BULBS.SDR CALA2013101692111Vsi · malfunctionedCAPTS VSI OFF FLAG & ERRATIC INDICATOR RTFL. REPLACED CAPTS VSI IAW B757 AMM 34-22-06. PERFORMED LT IRU OPERATIONS CHECKED IAW 34-21-00 & LT AIR DATA COMPUTER TESTED NORMAL.SDR CALA2013101592078Lanyard · unsecureL2 DOOR WILL NOT ARM. SECURED LOOSE LANYARD IN POUCH. ARM DISARM FUNCTION NOW NORMAL, SLIDE LIGHT CHECKED OKAY.SDR CALA2013101692112Minitel · defectiveNR 1 PILOT'S HEADSET IS DEFECTIVE. SPARE MINITEL USED, REPLACED MINITEL.SDR CALA2013101792150Pump · failedRT ENGINE HYD PUMP EICAS MESSAGE. TURNED OFF & VERIFIED NO RT SYSTEM PRESSURE. REPLACED RT ENGINE DRIVEN PUMP. RAN ENG IAW JRH 2-5-8, OPS CHECKED NORMAL.SDR CALA2013101492038Adc · faultyELEV ASYMMETRICAL STATUS MESSAGE WILL NOT CLEAR. REPLACED RT AIR DATA COMPUTER DUE TO FAULT SET ON RT SAM MODULE. ELEV ASYMMETRICAL MESSAGE GONE. ACCOMPLISHED SUCCESSFUL CURRENT STATUS TEST 30, AIRCRAFT REMAINS FULL CAPABILITY.SDR CALA2013101692106Starter · faultyAPU FAULT WILL NOT START. LAST 5 STARTS APUC SHOWED START ABORT, 11% N1, BATTERY VOLTAGE DURING CRANK WAS 22 VOLTS DURING MX START ATTEMPT. APU DOOR NOT DISPLAYED. APU, REPLACED STARTER & STARTER CLUTCH ASSEMBLY, OPERATIONAL CHECKED GOOD.SDR CALA2013101692117Seal · leakingNR 1 ENG OIL CONSUMPTION HAS REACHED AMBER LEVEL. FOUND STARTER DRIVE PAD SEAL LEAKING. REPLACED PAD SEAL IAW 72-61-02, NO LEAKS NOTED. REPLACED NR 1 ENG STARTER PRECAUTIONARY.SDR CALA2013101692119Headset · faultyCAPT HEADSET MIC IS HOT IN FLT INPH & SERV INPH, REPEAT WRITEUP. REPLACED CAPTS HEADSET, OPERATIONS CHECKED GOOD.SDR CALA2013101492017Plate · corrodedFRETTING CORROSION ON METAL FLOOR & ATTACHED FITTING BETWEEN BS1681 & BS 1720, RBL48 & RBL57. REMOVED CORROSION AT AFT DECK PLATE BS 1681 TO 1720 RBL48-57 IAW SRM 51-10-02. FOUND 3 ARE AS OUT OF LIMITS AT STATION 1692.2 RBL 50.2, STATION 1696.8 RBL 50.2, STATSDR CALA2013101592073Panel · damagedRT WING UNDERWING DAMAGED PANEL. REMOVED & BROUGHT INTO THE READY ROOM FOR REPAIR IAW NR 2 ENG INBD REV DAMAGE.SDR CALA2013101191956Skin · cracked2 INCH CRACK ON R4 DOOR INNER SKIN 10 INCHES FROM FWD EDGE & 31 INCHES FROM TOP EDGE. CUTOUT DAMAGE AREA ON R4 DOOR INNER SKIN 10 INCHES FROM FWD EDGE & 31" FROM TOP EDGE. FABRICATED DOUBLER & SHIM, INSTALLED IAW SRM 20-41-02 & 51-70-13 FIG 1.SDR CALA2013101191957Skin · dentedLOWER FUSELAGE SKIN BETWEEN BS680-694 BETWEEN STRINGER 22L & 24L HAS DENT FROM THE INSIDE OUT. REPAIRED LOWER FUSELAGE SKIN BS685-694 BETWEEN STRINGER 23L & 24L IAW ECRA5330-04729.SDR CALA2013101191958Skin · damagedFUSELAGE SKIN REPAIR AT BS685-694 BETWEEN STRINGER 22L & 24L IS CAT 'B' REPAIR. ACCOMPLISHED EXTERNAL FUSELAGE SKIN REPAIR BS685-694 BETWEEN STRINGER 22L & 24L IAW ECRA5330- 04729.SDR CALA2013101191970Lens · broken1ST CLASS EMERGENCY EXIT FLOOR LIGHT CLEAR COVER BROKEN & NEEDS TO BE REPLACED. REPLACED EMERGENCY EXIT LIGHT STRIP CLEAR LENS COVER AS REQUIRED.SDR CALA2013101191974Controller · inoperativeCOMPARTMENT TEMP INOPERATIVE LIGHT ALL 3. REPLACED ZONE TEMP CONTROLLER & OPERATIONS CHECKED GOOD.SDR CALA2013101191973Eec · failedLEFT ENGINE EEC MALFUNCTIONED. REPLACED EEC IAW MM 73-21-04 AND ACCOMPLISHED NR 1 ENGINE RUN. NO STATUS MESSAGE ON SHUTDOWN.SDR CALA2013100991890Processor · faultyCENTER FUEL TANK IND BLANK & TOTALIZER BLANK EICAS MESSAGE FUEL QTY IND. TOTALIZER & CALCULATOR DIFFERED GREATLY, LT & RT TANKS FLUX FROM 4000-6000LBS INDICATION. CENTER BLANKED OUT & IT WAS EMPTY. DURING DESCENT TOTALIZER & CALCULATOR INDICATIONS GRADUALLYSDR CALA2013100991891Floor Panel · damagedFLIGHT ATTENDANT REPORTS FLOOR SOFT AT ROW 4. MUSHY FLOOR PANEL FWD CABIN FLOOR. BEGAN REMOVAL OF FLOOR PANEL IN FWD CABIN, ALL SCREWS REMOVED. PANEL LEFT IN PLACE FOR SAFETY. NEW PANEL ON AOG.SDR CALA2013100991894Battery · faultyAPU NO START, 2 ATTEMPTS WITH FAULT BOTH TIMES. APU VERY SLOW TO SPOOL, ABORTS AT 19 PERCENT ON 3 TRIES. REPLACED APU BATTERY, WAS READING LOW VOLTAGE 21 BEFORE START & 11 VOLTS DURING START. REPLACED APU BATTERY IAW AMM, CHECKED GOOD. APU STARTS & RUNS NOSDR CALA2013101091940Feeder Cable · damagedEMERGENCY EXIT LIGHT STRIPS INOPERATIVE FROM ROW 8 THRU ROW 12. THE IN TRACK FEEDER CABLE IS OPEN. IN ADDITION, AT LEAST 2 ILLUMINATED STRIPS ARE INOPERATIVE. SPLICED IN FEEDER CABLE & REPLACED TRACK COVER. TESTED IAW AMM 33-51-96, 801, 401. ACCOMPLISHED SDR CALA2013101091950O-Ring · damagedON WALK AROUND FLT CREW REPORTS NR 1 ENG STRUT DRAIN LINE, LARGE LINE NR 2 LEAKING. REPLACED O-RING ON UPPER INBD HYD UNION ON THRUST REVERSER DIRECTIONAL CONTROL VLV. OPERATION CHECKED RAN REVERSER SEVERAL TIMES, NO LEAKS NOTED. NR 1 ENG OIL LEAKING, REPLSDR CALA2013101091951Starter · seizedRT ENG HUNG START THEN RT ENG STARTER EICAS ON 2ND ATTEMPT. FOUND NR 2 ENG STARTER SEIZED. INSP GEARBOX AFTER OLD STARTER OFF, NO DAMAGE FOUND. INSTALLED NEW STARTER, OPERATIONS CHECKED GOOD. SECURED NR 2 ENGINE FAN COWLING.SDR CALA2013100991886Plug · looseHYD FLUID LEAKING FROM LT WING OTBD SPOILER ACTUATOR. FOUND UPPER PLUG ON ACTUATOR LOOSE. SECURED & LEAK CHECKED. NO LEAKS NOTED.SDR CALA2013100991887Cover · missingCOVER ON EXIT LT MISSING AT DOOR 4R. REPLACED LENS COVER SECURE.SDR CALA2013100991888Light · looseEMERGENCY EXIT LIGHT STRIP LOOSE ROW 12-12 LT SIDE. LIGHT STRIP AT ROW 12 THRU 13 REINSTALLED & SECURED, OPERATIONS CHECKED GOOD.SDR CALA2013100991893Apu · malfunctionedAPU WILL NOT START, HANGS AT 28%. START ABORT MESSAGE. REPLACED APU.SDR CALA2013100991906Fan · noisyRT RECIRCULATING FAN EXCESSIVELY NOISY INTERFERES WITH COCKPIT COMM. RECIRCULATING MESSAGE ON EICASSDR CALA2013100791813Switch · faultyCOCKPIT DOOR DENY SW ROTATES 360 DEGREES & DOESN'T DENY ENTRY.SDR CALA2013100891844Girt Bar · out of adjustDOOR 1L ARMING LEVER VERY DIFFICULT TO OPERATE FOR ARMING & DIS-ARMING. ADJUSTED GIRT BAR, OPERATION CHECKED OKAY.SDR CALA2013100891845B-Nut · looseHYDRAULIC LEAK EVIDENCE UNDER RT WING RT AILERON. ACCOMPLISHED OPERATIONAL CHECK OF RT AILERON SYSTEM. TIGHTENED AILERON B-NUT UNIONS, NO LEAKS NOTED IAW AMM-29-00-99.SDR CALA2013100891846Fluid · leakingFLUID UNDER RT HORIZONTAL STAB & UNDER FUSELAGE. REMOVED PANEL TO CHECK PCU'S. OPERATED ALL THREE SYSTEMS & OPERATED ELEVATOR SEVERAL TIMES, NO ACTIVE LEAKS FOUND. ALL HYDRAULIC QTYS OKSDR CALA2013100991892Actuator · malfunctionedAPU DOOR FAULT, APU NO START. DOOR WOULD NOT OPEN, MESSAGE ON BOX DOOR ACTUATOR. APU CONSIDERED INOPERATIVE DUE TO DOOR ACTUATOR MESSAGE DEFERRAL. REPLACED APU AIR INTAKE DOOR ACTUATOR IAW MM, OPERATIONS CHECKED NORMAL..SDR CALA2013100891829Cover · damagedEMERGENCY FLOOR LIGHT COVER IS DAMAGED FROM ROWS 8ABC - 14ABC. REPLACED LIGHT COVER.SDR CALA2013100891830Cover · damagedEMERGENCY FLOOR LIGHT COVER IS DAMAGED FROM ROWS 37ABC- 40ABC. REPLACED LIGHT COVER.SDR CALA2013100891831Cover · damagedEMERGENCY FLOOR LIGHT COVER IS DAMAGED AT ROW 29ABC. REPLACED & SECURED COVER, OPERATION CHECKED GOOD.SDR CALA2013100791774Rivet · looseFIRST OFFICER`S ELEVATOR CONTROL AFT QUADRANT ASSEMBLY 251N2061-26 HAS PLAY AT THREE EACH RIVETS, SEE CMM 27-31-70 PG1010. REMOVED FWD & RT HAND RIVET & REAMED HOLES TO .260 INCHES IAW ECRA 2731-01384 & CMM 27- 31-70. REPLACED FASTENER OPERATIONS CHECKED OK SDR CALA2013100791777Wire · chafedWHILE ACCOMPLISHING LM7397, FOUND 1 BROKEN & 1 CHAFFED WIRE ON HARNESS TO PMA STATOR. ON NR 1 ENG REPLACED WIRE FROM CONNECTOR D4856 OF NR 1 EEC TO CONNECTOR D4858 OF THE PMA IAW WDM.
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